# Airworthiness Directives; Saab AB, Saab Aeronautics (Type Certificate Previously Held by Saab AB, Saab Aerosystems) Airplanes
> **Rule** · Final rule. · Published 2016-09-08 · Effective 2016-10-13 · 81 FR 61996
## Document
- **Document number:** 2016-20711
- **Category:** airworthiness
- **Type:** Rule
- **Action:** Final rule.
- **Citation:** 81 FR 61996
- **Publication date:** 2016-09-08
- **Effective date:** 2016-10-13
- **FAA docket:** Docket No. FAA-2016-6668
## Abstract

We are adopting a new airworthiness directive (AD) for certain Saab AB, Saab Aeronautics Model SAAB 2000 airplanes. This AD was prompted by a report that on some airplanes, during the paint removal process for repainting the airplane, the basic corrosion protection (anodizing and primer) coating was sanded down to bare metal on the aluminum skin panels, and the bare metal might not have been treated correctly for corrosion prevention. This AD requires an inspection of structural components of the airplane for any damaged protective coating; inspections of those areas for pitting corrosion, if necessary; a thickness measurement to determine if there is reduced skin thickness, if necessary; and repair, if necessary. We are issuing this AD to detect and correct damaged protective coatings. This condition could result in pitting corrosion damage; and reduced metal thickness, which could result in reduced static and fatigue strength of the airplane's structural parts.

## Source
- [Federal Register document](https://www.federalregister.gov/documents/2016/09/08/2016-20711/airworthiness-directives-saab-ab-saab-aeronautics-type-certificate-previously-held-by-saab-ab-saab)
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